Jovian tour design for orbiter and lander missions to Europa
Authors:
- Stefano CampagnolaSCStefano Campagnola
- Brent B. BuffingtonBBBrent B. Buffington
- Anastassios E. PetropoulosAPAnastassios E. Petropoulos
- 1 July 2014
- journal article
- Published by Elsevier in Acta Astronautica
- Vol. 100, 68-81
Abstract
No abstract availableKeywords
This publication has 20 references indexed in Scilit:
- Flybys in the planar, circular, restricted, three-body problemCelestial Mechanics and Dynamical Astronomy, 2012
- Europa Orbiter tour design with Io gravity assistsActa Astronautica, 2011
- Optimization of low-energy resonant hopping transfers between planetary moonsActa Astronautica, 2011
- A fast tour design method using non-tangent v-infinity leveraging transferCelestial Mechanics and Dynamical Astronomy, 2010
- Endgame Problem Part 2: Multibody Technique and the Tisserand-Poincare GraphJournal of Guidance, Control, and Dynamics, 2010
- Endgame Problem Part 1: V-Infinity-Leveraging Technique and the Leveraging GraphJournal of Guidance, Control, and Dynamics, 2010
- Automated Design of the Europa Orbiter TourJournal of Spacecraft and Rockets, 2002
- Graphical Method for Gravity-Assist Trajectory DesignJournal of Spacecraft and Rockets, 2002
- Europa's Differentiated Internal Structure: Inferences from Four Galileo EncountersScience, 1998
- V8 Leveraging for Interplanetary Missions: Multiple-Revolution Orbit TechniquesJournal of Guidance, Control, and Dynamics, 1997